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Recent Advancements in Fully Implicit Numerical Methods for Hypersonic Reacting Flows: With Application to Reentry and Arcjet ModelingNo abstract available
Document ID
20120015093
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Kirk, Benjamin S. (NASA Johnson Space Center Houston, TX, United States)
Stogner, Roy H. (Texas Univ. Austin, TX, United States)
Oliver, Todd A. (Texas Univ. Austin, TX, United States)
Bauman, Paul T. (Texas Univ. Austin, TX, United States)
Date Acquired
August 26, 2013
Publication Date
September 26, 2012
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
JSC-CN-26934
Report Number: JSC-CN-26934
Meeting Information
Meeting: Rocket Engine Modeling Symposium
Location: Tokyo
Country: Japan
Start Date: September 26, 2012
End Date: September 27, 2012
Sponsors: Japan Aerospace Exploration Agency
Funding Number(s)
WBS: WBS 747797.02.09.30.10
Distribution Limits
Public
Copyright
Public Use Permitted.

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